Invention Grant
- Patent Title: Flowpath component for a gas turbine engine including a chordal seal
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Application No.: US15267632Application Date: 2016-09-16
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Publication No.: US10329937B2Publication Date: 2019-06-25
- Inventor: Mark A. Boeke , Jeffrey J. DeGray , Richard M. Salzillo, Jr.
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C3/04
- IPC: F02C3/04 ; F01D11/00 ; F01D5/06 ; F01D9/04
Abstract:
A flow path component includes a platform having at least one radially aligned face. A chordal seal extends axially from the radially aligned face. The chordal seal includes a first curved face configured to prevent edge line contact under deflection conditions while the flow path component is installed in an engine.
Public/Granted literature
- US20180080334A1 FLOWPATH COMPONENT FOR A GAS TURBINE ENGINE INCLUDING A CHORDAL SEAL Public/Granted day:2018-03-22
Information query
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